A fault tolerant single sided matrix converter for flight control actuation systems

Xiao Yan Huang; Mao Jing Jin; Jian Cheng Zhang; Qin Fen Lu; You Tong Fang; Andrew Goodman; Chris Gerada

doi:10.1631/jzus.C1200164

A fault tolerant single sided matrix converter for flight control actuation systems

Xiao Yan Huang, Mao Jing Jin, Jian Cheng Zhang, Qin Fen Lu, You Tong Fang, Andrew Goodman, Chris Gerada

Research output: Journal Publication › Article › peer-review

Abstract

We describe a single sided matrix converter (SSMC) designed for safety critical applications like flight control actuation systems. Dynamic simulations of multi-phase SSMC using Matlab Simulink are carried out to evaluate the fault tolerance capabilities. Investigation into different numbers of phases and power converter topologies under single phase open circuit, single switch open circuit, and single switch short circuit has been executed. The simulation results confirm 5-phase SSMC design as a compromise between fault tolerance and converter size/volume. A 5-phase SSMC prototype was built. Experimental results verify the effectiveness of our design.

Original language	English
Pages (from-to)	866-874
Number of pages	9
Journal	Journal of Zhejiang University: Science C
Volume	13
Issue number	11
DOIs	https://doi.org/10.1631/jzus.C1200164
Publication status	Published - Nov 2012
Externally published	Yes

Keywords

Fault tolerance
Flight control actuation systems
Single sided matrix converter

ASJC Scopus subject areas

General Engineering

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10.1631/jzus.C1200164

Cite this

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title = "A fault tolerant single sided matrix converter for flight control actuation systems",

abstract = "We describe a single sided matrix converter (SSMC) designed for safety critical applications like flight control actuation systems. Dynamic simulations of multi-phase SSMC using Matlab Simulink are carried out to evaluate the fault tolerance capabilities. Investigation into different numbers of phases and power converter topologies under single phase open circuit, single switch open circuit, and single switch short circuit has been executed. The simulation results confirm 5-phase SSMC design as a compromise between fault tolerance and converter size/volume. A 5-phase SSMC prototype was built. Experimental results verify the effectiveness of our design.",

keywords = "Fault tolerance, Flight control actuation systems, Single sided matrix converter",

author = "Huang, {Xiao Yan} and Jin, {Mao Jing} and Zhang, {Jian Cheng} and Lu, {Qin Fen} and Fang, {You Tong} and Andrew Goodman and Chris Gerada",

note = "Funding Information: ‡ Corresponding author * Project supported by the UK government under the DTI CARAD program, the National Natural Science Foundation of China (No. 51007078), the National Key Technology Research and Development Program of the Ministry of Science and Technology of China (No. 2009BAG12A05), and the National High-Tech R & D (863) Program of China (No. 2011AA11A101) {\textcopyright} Zhejiang University and Springer-Verlag Berlin Heidelberg 2012",

year = "2012",

month = nov,

doi = "10.1631/jzus.C1200164",

language = "English",

volume = "13",

pages = "866--874",

journal = "Journal of Zhejiang University: Science C",

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AU - Huang, Xiao Yan

AU - Jin, Mao Jing

AU - Zhang, Jian Cheng

AU - Lu, Qin Fen

AU - Fang, You Tong

AU - Goodman, Andrew

AU - Gerada, Chris

N1 - Funding Information: ‡ Corresponding author * Project supported by the UK government under the DTI CARAD program, the National Natural Science Foundation of China (No. 51007078), the National Key Technology Research and Development Program of the Ministry of Science and Technology of China (No. 2009BAG12A05), and the National High-Tech R & D (863) Program of China (No. 2011AA11A101) © Zhejiang University and Springer-Verlag Berlin Heidelberg 2012

PY - 2012/11

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N2 - We describe a single sided matrix converter (SSMC) designed for safety critical applications like flight control actuation systems. Dynamic simulations of multi-phase SSMC using Matlab Simulink are carried out to evaluate the fault tolerance capabilities. Investigation into different numbers of phases and power converter topologies under single phase open circuit, single switch open circuit, and single switch short circuit has been executed. The simulation results confirm 5-phase SSMC design as a compromise between fault tolerance and converter size/volume. A 5-phase SSMC prototype was built. Experimental results verify the effectiveness of our design.

AB - We describe a single sided matrix converter (SSMC) designed for safety critical applications like flight control actuation systems. Dynamic simulations of multi-phase SSMC using Matlab Simulink are carried out to evaluate the fault tolerance capabilities. Investigation into different numbers of phases and power converter topologies under single phase open circuit, single switch open circuit, and single switch short circuit has been executed. The simulation results confirm 5-phase SSMC design as a compromise between fault tolerance and converter size/volume. A 5-phase SSMC prototype was built. Experimental results verify the effectiveness of our design.

KW - Fault tolerance

KW - Flight control actuation systems

KW - Single sided matrix converter

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ER -

A fault tolerant single sided matrix converter for flight control actuation systems

Abstract

Keywords

ASJC Scopus subject areas

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